N136EV
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
149 reports on file, 2011-02-28 – 2025-08-28.
Part: FITTING — CRACKED (ZONE 800) · airframe 37,166 hrs · 27,207 cycles
IN REF TO NRC 0087: AFTER AFT HANDRAIL SUPPORT FITTINGS REMOVAL, CRACK ON PASSENGER DOOR STAIR AFT SIDE PANEL WAS FOUND. PASSENGER DOOR STAIR AFT SIDE PANEL WAS REPAIRED PER CRJ 900 SRM 52-11-04-201-004-A01
Part: FITTING — CRACKED (ZONE 800) · airframe 37,166 hrs · 27,207 cycles
IN REF TO NRC 0087: AFTER FWD HANDRAIL SUPPORT FITTINGS REMOVAL, CRACK ON PASSENGER DOOR STAIR FWD SIDE PANEL WAS FOUND. PASSENGER DOOR STAIR FWD SIDE PANEL WAS REPAIRED PER CRJ 900 SRM 52-11-04-201-004-A01
Part: ACCESS PANEL — CORRODED (ZONE 100) · airframe 37,166 hrs · 27,207 cycles
INITIAL INSPECTION: CORROSION / CHAFE DAMAGE AT ALL SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB. CORROSION / CHAFE DAMAGE AT ALL SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 ALSO STRAP WAS EVALUATED OUT LMITIS AND WAS REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 51-42-10-001-001-A01
Part: BRACKET — WORN (ZONE 800) · airframe 37,166 hrs · 27,207 cycles
INITIAL INSPECTION: WEAR AT FWD / AFT HANDRAIL SUPPORT FITTINGS AND ALSO MISSING BUMPERS. WEAR AT FWD / AFT HANDRAIL SUPPORT FITTINGS WAS EVALUATED DUE EXESSIVE DAMAGE AND WAS REPLACED ALSO MISSING BUMPERS WAS INSTALLED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 51-42-21-001-001-A01
Part: SUPPORT — WORN (ZONE 500) · airframe 37,166 hrs · 27,207 cycles
WEAR ON PLATE SUPPORT OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: FITTING — WORN (ZONE 500) · airframe 37,166 hrs · 27,207 cycles
WEAR ON FLAP FITTING OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). FLAP FITTING OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-21-001-001-A01
Earlier reports · 2011–2024 · 143 reports
2024
Part: DOOR FRAME — CRACKED (ZONE 800)
R/H AFT EMERGENCY EXIT DOOR SH670-36600 SN SB0938 HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16488 REV IR DATED 5/8/2024.
Part: DOOR FRAME — CRACKED (ZONE 800)
R/H FWD EMERGENCY EXIT DOOR SH670-36600 SN SB0939 HAS A VISIBLE CRACK BELOW UPPER FWD AND AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16484 REV IR DATED 5/13/2024.
Part: DOOR FRAME — CRACKED (ZONE 800)
L/H FWD EMERGENCY EXIT DOOR SH670-36600 SN SB0940 HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-164870 REV IR DATED 5/7/2024.
Part: LUG — CRACKED (ZONE 800)
L/H AFT EMERGENCY DOOR SH670-36600 SN SB0937 HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16486 REV IR DATED 5/7/2024.
2022
Part: SKIN — CORRODED · airframe 30,089 hrs · 21,137 cycles
PAX DOOR INNER SKIN CORRODED AROUND PANEL CUTOUTS NUMEROUS LOCATIONS. TCI: 52-10-301 - REMOVED UNSERVICABLE PAX DOOR INNER SKIN AND INSTALLED SERVICABLE INNER SKIN IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01,51-42-21-001-001-A01, 51-40-11-001-001-A01 AND 51-42-22-001-001-A01.
Part: WEB — CORRODED · airframe 30,089 hrs · 21,137 cycles
PAX DOOR FWD WEB CORRODED AROUND ACCESS PANEL CUTOUTS AND NUTPLATES - REMOVED ANLGES AND FITTIGNS FROM UNSERVICABLE WEB. LOCATED AND REINSTALLED SAME SERVICEABLE ANGLE AND FITTING ON SERVICEABLE WEB P/N 601R317071-12 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: FRAME — CHAFED · airframe 30,089 hrs · 21,137 cycles
FRAME, PN: MM670-36213-009, AT FS 1144 IN BETWEEN STGRS 9L & 10L HAS DAMAGE FROM HYD LINE CONTACT. - REPAIRED FARME @FS1144 BETWEEN STGR 9L & 10L IAW ENDEAVOR EA CRJ 952 12884 DATED 2-22-22 REV EA --REF JOB: 81522661 OP 525 FOR ACCUMULATOR INSTALLATION/REMOVAL
Part: ANGLE — CRACKED · airframe 30,089 hrs · 21,137 cycles
POWER ASSIST MOTOR STIFFENING ANGLE CRACKED. - REMOVED AND REPLACED POWER ASSIST MOTOR STIFFENING ANGLE P/N: 601R317745-7 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: MOUNT — CHAFED · airframe 30,089 hrs · 21,137 cycles
LH ENGINE MOUNT YOKE FOUND TO HAVE CHAFING IN ATTACHMENT PIN LADIUS MARKED WITH RED TAPE. - REPAIRED LH ENGINE YOKE IAW MHIRJ REO 670-71-21-057 REV-- DATED 2013- AND REO 690-71-21-035 REV-- DATED 2022-03-01.
Part: NONE — CORRODED · airframe 30,089 hrs · 21,137 cycles
FOUND CLIP P/N: 601R319034-2 TO BE CORRODED TOWARDS THE HINGE - REPLACED CLIP P/N: 601R319034-2 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01
Part: WEB — CRACKED · airframe 30,089 hrs · 21,137 cycles
PAX DOOR AFT WEB CRACKED ON BOTTOM BY SUPPORT ANGLE - REMOVED ANGLES AND FITTINGS FROM UNSERVICEABLE WEB. LOCATED AND REINSTALLED SAME SERVICEABLE ANGLE AND FITTING ON SERVICEABLE WEB P/N: 601R317071-11 IAW CRJ900 SRM 51-40-11-001-001-A01 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: LUG — DAMAGED · airframe 30,089 hrs · 21,137 cycles
RH AILERON HAS DAMAGE TO LUGS MARKED C AND E. - REPAIRED DAMAGE TO RH AILERON LUGS MARKED C AND E IAW BOMBARDIER REO 670-57-61-237 REV -- DATE 2017-07-25
Part: SLEEVE — CORRODED · airframe 30,089 hrs · 21,137 cycles
PAX DOOR TENSION TIES BUSHINGS AND BUSHING SLEEVES CORRODED - REMOVED AND REPLACED TENSION TIE BEARINGS SLEEVE P/N MS17796-106 (2EA) AND SPACER SLEEVE P/N NAS43HT16-56 (2EA) IAW CRJ900 AMM 52-11-19-000/400-801-A01.
Part: RETAINER — DAMAGED · airframe 30,089 hrs · 21,137 cycles
FOUND BOTTOM SEAL RETAINER P/N: 601R318722-1 DAMAGED - REPLACED BOTTOM SEAL RETAINER P/N: 601R318722-1 IAW CRJ900 SRM 51-42-06-001-001-A01 51-40-11-001-001-A01
Part: LUG — DAMAGED · airframe 30,089 hrs · 21,137 cycles
LH AILERON HAS DAMAGE TO LUGS MARKED D. - REPAIRED DAMAGE TO LH AILERON LUG MARKED IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25
Part: FRAME — CORRODED · airframe 30,089 hrs · 21,137 cycles
FS 349 LOWER FRAME SEGMENT CORRODED BETWEEN STGR 25L AND STGR 25R. - REPAIRED FRAME 349 LOWER SEGMENT STGR 25L-25R IAW ENDEAVOR EA CRJ953-12888, REV IR DATED 2/22/22.
Part: FRAME — CORRODED · airframe 30,089 hrs · 21,137 cycles
FS333 LOWER FRAME SEGMENT CORRODED BETWEEN STGR 25L AND STGR 25R. - FOUND TO BE BEYOND REPAIRABLE LIMITS IAW CRJ 900 SRM 53-00-06-201-005-A01, REPAIRED FRAME IAW CRJ 900 SRM 53-00-06-201-006-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01 AND 51-21-11-001-001-A01
Part: ANGLE — CRACKED · airframe 30,089 hrs · 21,137 cycles
LH VERTICAL STAB DRAG ANGLE HAS SUSPECTED CRACK. - REMOVED AND REPLACED DRAG ANGLE IAW CRJ 900 SRM 51-42-22-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01
Part: CLEAT — CORRODED · airframe 30,089 hrs · 21,137 cycles
FOUND CLEAT P/N: 600-31902-269 CORRODED AT FS313.56 DD4. - REMOVED AND REPLACED CLEAT P/N 600-13902-269 AT FS 313.56 DD4 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-0A1.
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL AT DD6 CORRODED - REMOVED AND REPLACED INTERCOSTAL PN 601R318057-APO BRACKET P/N 601R31902-461 AT DD6 IAW CRJ900 SRM 51-42-06-001-001-A01 51-40-11-001-001-A01 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
PAX DOOR INTERCOSTAL DD4 IS CORRODED. TCI: 52-10-301. - REMOVED AND REPLACED INTERCOSTAL P/N 601T318093-1 AND BRACKET P/N 601R31902-461 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 (DD4).
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL 27R CORRODED BETWEEN FS 394 AND FS 409. - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-21-11-001-001-A01
Part: NONE — NONE · airframe 30,089 hrs · 21,137 cycles
FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 581.00 AND FS 661.00+32 IS CORRODED. - REMOVED, FABBED & INSTALLED SEAT TRACK IAW CRJ 900 SRM 51-40-11-001-001-A01 & AMM 53-00-49-000/400-801-A01.
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL 27L CORRODED BETWEEN FS 394 AND FS 409. - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-00-001-001-A01, 51-23-00-001-001-A01, 51-21-11-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL 27L CORRODED BETWEEN FS 349 AND FS 364. - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01 AND 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
PAX DOOR INTERCOSTAL DD5 IS CORRODED. - REMOVED AND REPLACED INSTERCOSTAL P/N 601R318091-5 AND BRACKET P/N 601R31902-461 AT DD5 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: NONE — CORRODED · airframe 30,089 hrs · 21,137 cycles
RH FLOOR SILL BETWEEN FS 280.00 TO FS 319.00 IS CORRODED IN MULTIPLEL LOCATIONS - REMOVED AND REPLACED FLOOR SILL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-10-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL AT STGR 21L IS CORRODED BETWEEN FS310 AND FS349. TCI: 53-20-304 - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 53-21-23-101-001-A02, 51-21-06-001-001-A01, 51-21-11-001-001-A01 INSTALLED AVIONICS SHELF AT F.S. 310 TO F.S. 349 IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: ANGLE — CORRODED · airframe 30,089 hrs · 21,137 cycles
TOP ANGLE CLOSEST TO HINGE AND CLIPS CORRODED - REMOVED AND REPLACED ANGLE P/N 601R317052-1 AND CLIP (1EA) P/N 601R318058-1 AT CODDER CENTER OF PAX DOOR CLOSEST TO HINGE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: ANGLE — CORRODED · airframe 30,089 hrs · 21,137 cycles
AVI BAY FLOORBOARD SUPPORT ANGLE ON FS 280 LOWER FRAME SEGMENT IS CORRODED. - BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-21-06-001-001-A01, 53-00-00-101-001-A01, 51-21-11-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL AT DD7 CORRODED - REMOVED AND REPLACED INTERCOSTAL P/N 601R318826-1 AND CUP P/N 601R318824-1 AT DD7 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
LH SIDE SEAT TRACK AT FS847+16-905 HAS MULTIPLE SPOTS OF CORROSION - REMOVED AND REPLACED SEAT TRACK IAW CRJ900 AMM 53-00-49-000/400-801-A01
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 485.00 AND FS 581.00 IS CORRODED. - REMOVED FASTENERS & CORRECTED COUNTERSINKS & REINSTALLED FASTENERS IAW CRJ 900 SRM 51-40-11-001-001-A01 & 53-00-49-400-801 (CONFIG A11).
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
LH SIDE SEAT TRACK AT FS 785-847+16 HAS MULTIPLE SPOTS OF CORROSION - REMOVED AND REPLACED SEAT TRACK IAW CRJ900 SRM 53-00-49-201-002-A01, 51-40-11-001-001-A01 AND AMM 53-00-49-000/400-801-A11
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL 27R CORRODED BETWEEN FS 349 AND FS 364. - REMOVED AND REPLACED INTERCOSTAL 27R IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01 AND 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
RH SIDE SEAT TRACK OF FS570-661+16 HAS MULTIPLE SPOTS OF CORROSION - REMOVED AND REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A11
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
SIDE SEAT TRACK AT FS744.15-761.85 HAS MULTIPLE SPOTS OF CORROSION. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A11. PN SH690-36285-1.
Part: INTERCOSTAL — CORRODED · airframe 30,089 hrs · 21,137 cycles
INTERCOSTAL AT DD7A CORRODED - REMOVED AND REPLACED INTERCOSTAL P/N 601R318083-1 AND CUP P/N 601R318058-1 AT DD7A IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
SEAT TRACK FROM FS 847+16-985 RBL 9 HAS MULTIPLE SPOTS OF CORROSION - REMOVED, FABED, AND INSTALLED SEAT TRACK F/S 847+16 - 985 @ RBL9 IAW CRJ900 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A11
Part: STRINGER — CORRODED · airframe 30,089 hrs · 21,137 cycles
STRINGER 25R IS CORRODED BETWEEN FS280 AND FS 338. - REPAIRED STRINGER IAW ENDEAVOR AIR EA CRJ953-12914.
Part: CROSSBEAM — CORRODED · airframe 30,089 hrs · 21,137 cycles
FOUND LH FS 280 CROSSBEAM CORRODED AT MULTIPLE LOCATIONS. - REMOVED UNSERVICEABLE, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE PN CC670-34094J P-18. INSTALLED NEW SERVICEABLE FS 280 LH CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-010-A01, 51-42-13-001-001-A01.
Part: ANGLE — CORRODED · airframe 30,089 hrs · 21,137 cycles
FS 280.00 CROSS BEAM J ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9. - REMOVED UNSERVICEABLE, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE FS 280 J ANGLE PN CC670-34095-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
Part: FORMER — CORRODED · airframe 30,089 hrs · 21,137 cycles
PAX DOOR AFT FORMER CORRODED. - LOCATED AND DRILLED NEW AFT FORMER P/N 601R318034-5 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW AFT FORMER CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7/25/20.
Part: ANGLE — CORRODED · airframe 30,089 hrs · 21,137 cycles
AFT FORMER SUPPORT ANGLE CORRODED. - LOCATED AND DRILLED NEW AFT FORMER SUPPORT ANGLE P/N 601R318732-3 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE CRJ 900 SRM 51-42-06-001-001-A01 REV 38 07/25/20.
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 485.00 AND FS 581.00 IS CORRODED. - REMOVED CORRODED SEAT RAIL AT LBL 9 BETWEEN 485.00 TO FS 581 IAW CRJ AMM 53-00-49-000-801-A11 LOCATED & DRILLED NEW SEAT RAIL AT FS 485.00 TO 581.00 IAW CRJ 900 SRM 53-00-49-201-002-A01 & INSTALLED NEW SEAT RAIL AT FS 485 TO FS 581 LBL 9 IAW CRJ 900 AMM 53-00-49-400-801-A11.
Part: ANGLE — CORRODED · airframe 30,089 hrs · 21,137 cycles
FWD SUPPORT ANGLE CORRODED. - LOCATED AND DRILLED NEW FWD FORMER SUPPORT ANGLE P/N 601R318737-3 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW SUPPORT ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20.
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
SEAT TRACK FROM FS 927-977 LBL 18 HAS MULTIPLE SPOTS OF CORROSION. - REMOVED AND REPLACED SEAT TRACK @ LBL 27 IAW CRJ 900 AMM 53-00-49-000/400-801-A11.
Part: BRACKET — CORRODED · airframe 30,089 hrs · 21,137 cycles
MACHINED FITTING LEFT OF STGR 23L AT FS 565.00 IS CORRODED - REMOVED AND DRILLED UP NEW PART INSTALLED SERVICEABLE MACHINE BRACKET P/N SH670-33390-2 AT STEP 23L AT FS 565.00 IAW CRJ 900 SRM 51-42-26-001-001-A01, 51-40-11-001-001-A01, 51-42-22-001-001-A01, AND 51-42-15-001-001-A01
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
LH SIDE SEAT TRACK AT FS 661+16-674 HAS MULTIPLE SPOTS OF CORROSION - REMOVED, FABBED AND INSTALLED L/H SIDE SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01 AND CRJ 900 AMM 53-00-49-000/400-801-A11
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
RH SIDE SEAT TRACK AT FS 661+16-674 HAS MULTIPLE SPOTS OF CORROSION - REMOVED, FAB'D AND INSTALLED SEAT TRACK IAW CRJ 900 SRM 53-00-49-201-002-A01 AND CRJ 900 AMM 53-00-49-000/400-801-A11
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
RH SIDE SEAT TRACK AT FS 469-485 HAS MULTIPLE SPOTS OF CORROSION - INSTALLED 'NEW' SEAT RAIL (P/N SH690-32233-3) R F/S-485 IAW CRJ 900 SRM 53-00-49-400-801(CONFIG A11)
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
SEAT TRACKS FROM FS 847+16-985 LBL 9 HAS MULTIPLE SPOTS OF CORROSION - INSTALLED 'NEW' SEAT TRACK (PN SH690-37388-5) F/S 847+16 - 985 LBL 9 CRJ 900 AMM 53-00-49-400-801(CONFIG A11)
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 661.00+32 AND FS 677.00 IS CORRODED TCI: 53-20-318 - LOCATED AND DRILLED NEW FLOOR SEAT TRACK PN: 20276-288-0-0A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 53-00-49-201-002-A01. INSTALLED SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801(CONFIG A11)
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
LH SIDE SEAT TRACK AT FS485-570 HAS MULTIPLE SPOTS OF CORROSION. - REMOVED AND REPLACED LH SIDE SEAT TRACK AT FS 485-570 IAW CRJ 900 AMM 53-00-49-000-801-A11, AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 349.00 AND FS 485.00 IS CORRODED. - REMOVED AND INSTALLED FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 349.00 AND FS 485 IAW CRJ AMM 53-00-49-000-801-A11 AND AMM 53-00-49-400-801-A11, IPC P/N: SH670-32159-1.
Part: BRACKET — CRACKED · airframe 30,089 hrs · 21,137 cycles
HYD SYS #2 OUTBOARD BRAKE ACCUMULATOR FWD INBOARD AND OUTBOARD MOUNTING BRACKET ARE CRACKED - R&R HYD SYS #2 ACCUMULATOR FWD INBOARD AND OUTBOARD MOUNT BRACKETS P.N. CC670-75604-3 AND CC67-75604-4 IAW CRJ 900 SRM 51-42-21-001-001-A01
Part: SEAT TRACK — CORRODED · airframe 30,089 hrs · 21,137 cycles
LH SIDE SEAT TRACK AT FS379-469 HAS MULTIPLE SPOTS OF CORROSION - REMOVED AND REPLACED SEAT TRACK IAW CRJ900 AMM 53-00-49-000/400-801-A11
2021
Part: GATE — CRACKED (PAX DOOR) · airframe 28,527 hrs · 19,757 cycles
PAX DOOR OUTER HANDLE FLAP CRANKED AT EDGE MARKED WITH YELLOW TAPE. REPLACED PAX DOOR OUTER HANDLE FLAP IAW CRJ 900 SRM 51-42-06-001-001-A01 & APPLIED PAINT IAW CRJ 900 SRM 51-25-01-001-001-A01.
2018
Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 23,607 hrs · 15,938 cycles
GEAR DESAGREE AFTER TAKE OFF, REMOVED AND REPLACED THE LDG GEAR SELECTOR VALVE ASSY IAW AMM 32-32-10, OPS CHECKED GOOD.
Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 23,320 hrs · 15,715 cycles
ROW 14 A+B PAX 02 MASK DEPLOYED. STOWED O2 MASK DOOR AT ROW 14AB, REF AMM 35-21-09.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 22,801 hrs · 15,337 cycles
LEFT HORIZONTAL STAB HAS TWO DENTS ON UPPER OUTBOARD SURFACE. 32 INCHES FROM TIP, 15 INCHES FROM THE LE. THE DENTS ARE .5 INCH IN DIAMETER. REPAIRED SKIN IAW REO 690-55-11-111.
2017
Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD LAVATORY) · airframe 22,038 hrs · 14,807 cycles
SMOKE DETECTOR IN THE FWD LAVATORY ACTIVATED DURING DESCENT. R & R THE FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD IAW AMM 26-16-00.
Part: SMOKE DETECTOR — DAMAGED (LAVATORY) · airframe 22,038 hrs · 14,807 cycles
AFT LAVATORY SMOKE DETECTOR ASSY HAS DAMAGE. REMOVED AND REPLACED AFT LAV SMOKE DETECTOR ASSY IN REF TO AMM 26-16-01-400-801 OPS CHECK GOOD IN REFERENCE TO AMM 26-16-00-710-801.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,330 hrs · 14,255 cycles
STRINGER 25L HAS CORROSION BETWEEN FS319-333. REMOVED AND INSTALLED NEW STRINGER 25L, FS319-FS333 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-31350.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,330 hrs · 14,255 cycles
STRINGER 26L HAS CORROSION BETWEEN FS333-349. REMOVED AND INSTALLED NEW STRINGER 26L, FS333-FS364 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-31350.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,330 hrs · 14,255 cycles
STRINGER 26R HAS CORROSION BETWEEN FS333-349. REMOVED AND INSTALLED NEW STRINGER 26R, FS333-FS364 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-31350.
Part: FRAME — CRACKED (FUSELAGE) · airframe 21,330 hrs · 14,255 cycles
UPON REMOVAL OF STRINGER 26R FOUND CRACK DAMAGE ON FRAME FS333 LOWER FLANGE BETWEEN STRINGER 26R AND STRINGER 25R. CUT OUT FRAME FLANGE IAW REO 670-53-21-1281. PERFORMED EDDY CURRENT INSPECTION OF CUT EDGES IAW NDTM PT 1, 51-20-006-250-A01. FABRICATE REPAIR PARTS IAW SRM 51-24-21-001-001-A01, 51-24-36-001-001-A01. DRILLED FASTENER HOLES AND INSTALLED FASTENERS IAW SRM 51-42-001-001-A01. COMPLIED WITH EC/TC REO 670-53-21-1281 AND GENERIC REO 670-53-21-1281 REV--, DATED: 04/11/2016 AS WRITTEN.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,330 hrs · 14,255 cycles
STRINGER 26R HAS CORROSION BETWEEN FS280-295 AND BETWEEN FS295-310. REMOVED AND REPLACED STRINGER 26R, FS280-FS333 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 21,330 hrs · 14,255 cycles
FS280 BUTT STRAP HAS CORROSION AT 26L-26R. BLENDED CORROSION ON FS280 BUTT STRAP, NTD, REMAINING MATERIAL IS .076, ORIGINAL THICKNESS WAS .080, .004 REMOVED. COMPLIED WITH EA 05-2017-065.
Part: BRACKET — BROKEN (HAND RAIL) · airframe 21,330 hrs · 14,255 cycles
AFT PAX DOOR HAND RAIL LUG BROKEN ON THE ANCHOR BRACKET. REMOVED AND REPLACED THE HAND RAIL ANCHOR LUG BRACKET IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND AMM 52-11-05-400-802,51-11-05-000-802-A01.
Part: INTERCOSTAL — CORRODED (BS 349-365) · airframe 21,330 hrs · 14,255 cycles
INTERCOSTAL STRINGER 27R HAS CORROSION BETWEEN BS 349 - 364. REMOVED, DRILLED, AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 21,330 hrs · 14,255 cycles
INTERCOSTAL AT STRINGER 27L HAS CORROSION BETWEEN BS 349 - 364. REMOVED, DRILLED, AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,884 hrs · 13,230 cycles
LEFT AFT OVER-WING EMERGENCY LIGHT OUT. RE-LAMPED LEFT AFT OVER-WING EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECKED GOOD.
Part: CHARGER — FAILED (CABIN) · airframe 19,802 hrs · 13,179 cycles
EMERGENCY CEILING LIGHTS IN FIRST CLASS INOP. REMOVED AND REPLACED NR 2 EPSU BATTERY CHARGER IAW AMM 33-51-17. OPS CHECK GOOD.
2015
Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 16,421 hrs · 10,806 cycles
MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRNG UNDER CEILING PANEL ROW 4 IAW ESPM 20-26-03.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 15,354 hrs · 10,073 cycles
LEFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. FOUND CONNECTOR TO BE DISCONNECTED. RECONNECTED IAW WM25-28-01. OPS TESTED GOOD IAW 33-51-000-710-801.
Part: FLOOR SUPPORT — CRACKED (BS 259-280) · airframe 15,347 hrs · 10,070 cycles
FOUND RT COCKPIT FLOOR SUPPORT ANGLE CRACKED. REMOVED FLOOR SUPPORT RBL 12, WL 72.5, BS 259.2 - 280 IAW SRM 51-42-06-001-001-A01. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33052.
Part: STRAP — CRACKED (FUSELAGE) · airframe 15,347 hrs · 10,070 cycles
FOUND JOINT STRAP TO BE CRACKED. REPAIRED IAW REO 690-53-82-052.
Part: SEAT TRACK — CORRODED (BS 752) · airframe 15,347 hrs · 10,070 cycles
SEAT TRACK AT BS 752.5 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW DWG 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A11 AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 720.85) · airframe 15,347 hrs · 10,070 cycles
RT SIDE SEAT TRACK CORRODED AT BS 720.85. REMOVED CORROSION. FOUND TO BE OUT OUT LIMITS IAW SRM 53-41-49-101-001-A01. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G. R & R THE SEAT TRACK IAW EC/TC REO 670-53-00-343 AND AMM 53-00-49-400-801, 53-00-49-000-801.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,348 hrs · 10,071 cycles
RT FLOORBEAM RBL 12 AT FS 280.00 CORRODED AT LOWER SECTION. EVALUATED, FLOOR POST FOUND TO BE EXTMELY EXFOLIATED AND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED THE FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A10, 51-42-21-001-001-A01, 51-42-10-001-001-A01 AND INSTALLED IAW SRM 51-42-06-001-001-A01,51-42-21-001-001-A01, DWG 690-53-11-480. COMPLIED WITH REO 690-53-11-736.
Part: SKIN — CHAFED (LT WING) · airframe 15,347 hrs · 10,070 cycles
LT WING SKIN PANEL 584EB FOUND CHAFED. BLENDED DAMAGE IAW SRM 51-12-00-001-001-A01 FOUND TO BE OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. RECEIVED AND COMPLIED WITH ECTC EA 32-2015-026.
Part: SEAT TRACK — CORRODED (BS 752) · airframe 15,347 hrs · 10,070 cycles
SEAT TRACK AT BS 752.50 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW AMM 53-41-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-801-A11.
Part: SEAT TRACK — CORRODED (BS 797) · airframe 15,347 hrs · 10,070 cycles
SEAT TRACK AT BS 797 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-013, AMM 53-00-49-000-801, A11 AND AMM 53-00-49-400-801, -A11.
Part: FLOOR SUPPORT — CORRODED (BS 280-283.5) · airframe 15,347 hrs · 10,070 cycles
RT FLOOR SUPPORT BS 280-283.5 HAS CORROSION ON PRIOR REPAIR DOUBLER. R & R CORRODED DOUBLER IAW SRM 51-42-06-001-001-A01. FABRICATED NEW REPAIR DOUBLER IAW SRM 51-21-16-001-001-A01, & SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 677-847) · airframe 15,347 hrs · 10,070 cycles
RBL 9, SEAT TRACK BS 677-847 CORRODED & FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013, REV J. R & R THE SEAT TRACK IAW AMM 53-00-49-000-/400-801. FABRICATED NEW SEAT RAIL IAW GREO 670-53-00-343 & DWG 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 15,347 hrs · 10,070 cycles
RBL9, SEAT TRACK BS 661+32-677 CORRODED & FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013, REV J. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A11 AND AMM 53-00-49-400-801, CONFIG A11.
Part: SEAT TRACK — CORRODED (BS 677-847) · airframe 15,347 hrs · 10,070 cycles
LBL 9, SEAT TRACK BS 677-847 CORRODED & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. R & R SEAT TRACK IAW AMM 53-00-49-000/400-801, A11.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,347 hrs · 10,070 cycles
LBL 9, SEAT TRACK BS 581 - 661+32 CORRODED & FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013, REV J. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A11 AND AMM 53-00-49-400-801, CONFIG A11.
Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 15,347 hrs · 10,070 cycles
LBL 9, SEAT TRACK BS 661+32-677 CORRODED & FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013, REV J. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A11 AND AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,347 hrs · 10,070 cycles
RBL 9, SEAT TRACK FS 581-661+32 CORRODED & FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013, REV J. R & R SEAT TRACK IAW AMM 53-00-49-000-801, A01/53-00-49-400-801-A01.
Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 15,347 hrs · 10,070 cycles
AFT CARGO DOOR LOWER SILL HAS CORROSION. REPAIRED IAW REO 670-53-61-913.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,347 hrs · 10,070 cycles
BS 280, FLOORBEAM CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 15,347 hrs · 10,070 cycles
RBL 9, SEAT TRACK SEGMENT BS 485-581 CORRODED. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013, REV J. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000, GREO 670-53-00-343, AND AMM 53-00-49-400-801.
Part: FLOOR SUPPORT — CORRODED (BS 349-357) · airframe 15,347 hrs · 10,070 cycles
RIGHT FLOOR SUPPORT CORRODED BS 349 - 357. REPAIRED IAW REO 670-53-00-390
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 15,347 hrs · 10,070 cycles
SEAT TRACK CORRODED BS 349-485, RBL 9. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, R & R THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, AND GREO 670-53-00-343.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,347 hrs · 10,070 cycles
COCKPIT FLOORBEAM AFT ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, DWG CCC670-34010, DWG CC670-33052, SRM 51-40-11-001-001-A1, 51-44-06-001-001-A01, AND DWG CC670-34095, REV.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,347 hrs · 10,070 cycles
CRAWLWAY FLOORBEAM ANGLE ON AFT SIDE OF FS 280 CORRODED. R & R THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34256, SHEET 1.
2014
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 13,623 hrs · 8,884 cycles
FWD CARGO AFT DOOR SEAL RETAINER DAMAGED AT AFT AND FWD CORNERS. COMPLIED WITH EC/TC REO 690-52-35-013 FOR THE PERMANENT REPAIR IAW REO 690-52-35-013, REV "A" ON THE FWD CARGO COMPARTMENT AFT DOOR SEAL. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3.
Part: RETAINER — DENTED (CARGO DOOR SEAL) · airframe 13,623 hrs · 8,884 cycles
FWD CARGO FWD DOOR SEAL RETAINER DAMAGED AT AFT AND FWD CORNERS. COMPLIED WITH EC/TC REO 690-52-35-013 FOR THE PERMANENT REPAIR IAW REO 690-52-35-013, REV. "A" ON THE FWD CARGO COMPARTMENT FWD DOOR SEAL. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 13,310 hrs · 8,672 cycles
AFT F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERIES IAW AMM 25-61-00. OPS CHECKED GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.
2013
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 12,362 hrs · 8,057 cycles
SERVICE DOOR UPPER EXIT LIGHT COVER CRACKED. R & R SERVICE DOOR UPPER EXIT LIGHT COVER IAW AMM 33-51-05.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 12,043 hrs · 7,863 cycles
MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14.
Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,356 hrs · 7,448 cycles
PHOTO LUMINESCENT STRIP MISSING AT SEAT 12 A/B. REPLACED MISSING PHOTOLUMINESCENT STRIP ESCAPE PATH MARKING IAW AMM 33-51-01. ACFT OK FOR SERVICE.
Part: FLOOR PANEL — DETERIORATED (COCKPIT) · airframe 11,282 hrs · 7,406 cycles
COCKPIT FLOOR PANEL IS SPONGY. REPAIRED IAW GREO 670-53-00-365. CLASSIFIED AS MAJOR IAW GMM 5-3.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 10,709 hrs · 7,044 cycles
CAPT SIDE COCKPIT FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN FLASHLIGHT AND OPS CHECKED GOOD IAW AMM 25-61-01.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 10,637 hrs · 6,991 cycles
SERVICE DOOR EXTERIOR EMERGENCY LIGHT FAILED. OPS CHECK FOUND RED CAP STILL ON CONNECTOR FOR EPSU BATTERY PACK CHARGER. RECONNECTED NR 2 EPSU BATTERY CHARGER IAW AMM 33-51-17-400-802. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-00-710-801.
Part: SKIN PANEL — UNSERVICEABLE (WING) · airframe 10,637 hrs · 6,991 cycles
PANEL 652JB HAS ONE BAD NUT PLATE. R & R NUTPLATE IAW SRM 51-42-06-001-001-A01. REPAIR CLASSIFIED AS A MAJOR.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 10,637 hrs · 6,991 cycles
FLOORBEAM AT FWD OF FRAME BS 280 AT BL 12.00 IS CRACKED AT THE POINT WHERE THE FLOORBEAM BACK UP BRACKET ATTACHER RT SIDE. REPAIRED IAW REO 690-53-11-450.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 10,637 hrs · 6,991 cycles
FLOORBEAM AT FWD OF FRAME BS 280 AT BL 12.00 IS CRACKED AT THE POINT WHERE THE FLOORBEAM BACK UP BRACKET ATTACHES LT SIDE. REPAIRED IAW REO 690-53-11-480.
Part: FLOOR SUPPORT — CRACKED (BS 276) · airframe 10,637 hrs · 6,991 cycles
COCKPIT FLOOR SUPPORT ANGLE AT LBL 12 IS CRACKED AT FS 276. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-001-001. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01.
Part: FLOOR SUPPORT — CRACKED (BS 276) · airframe 10,637 hrs · 6,991 cycles
COCKPIT FLOOR SUPPORT ANGLE AT RBL 12 IS CRACKED AT FS 276. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 10,637 hrs · 6,991 cycles
SERVICE DOOR LOWER SILL UPPER ANGLE CORRODED. REMOVED LOWER SILL UPPER ANGLE FROM SERVICE DOOR LOWER SILL ANGLE REQUIRES REPLACEMENT IAW SRM TASK 51-42-06-0001-001-A01, 51-42-20-001-001-A01. INSTALLED LOWER SILL UPPER ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.
Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 10,637 hrs · 6,991 cycles
PAX DOOR SURROUND MID CAP ANGLE CORRODED AT SCREW HOLES. REMOVED PAX DOOR SURROUND MID CAP ANGLE. CORRODED BEYOND LIMITS IAW 53-00-00-101-001-A01 SRM 57-41-02-001-001-A01. REPLACED PAX DOOR SURROUND MID CAP ANGLE IAW SRM 51-41-02-001-001-A01.
Part: WEB — CORRODED (BS 280) · airframe 10,637 hrs · 6,991 cycles
LT BS 280 WEB IS CORRODED AT LBL 9 AT FLOOR LEVEL. REMOVED SPLICE LT CUT LT BS 280 WEB IAW REO 670-53-11-594. FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-11-594.
Part: WEB — CORRODED (BS 280) · airframe 10,637 hrs · 6,991 cycles
RT BS 280 LOWER WEB IS CORRODED. R & R WEB IAW REO 670-53-11-594. COMPLIED WITH REO 670-53-11-594.
Part: FRAME — CORRODED (BS 333) · airframe 10,637 hrs · 6,991 cycles
FRAME BS 333 AT THE BOTTOM IS CORRODED. REMOVED CORRSION IAW SRM 51-21-06-001-001, ORIG MAT .050, DWG SH670-31356. COMPLIED WITH EO CL600-2024-53-I00204.
Part: CHANNEL — CORRODED (BS 295-310) · airframe 10,637 hrs · 6,991 cycles
LOWER TCAS CHANNEL BETWEEN BS 295 & 310 S27 CORRODED. REMOVED LOWER TCAS CHANNEL IAW SRM 51-42-06-001-001. INSTALLED NEW LOWER TCAS CHANNEL IAW SRM 51-42-21-001-001 AND 51-42-06-001-001.
Part: INTERCOSTAL — CORRODED (BS 364) · airframe 10,637 hrs · 6,991 cycles
INTERCOSTAL FWD OF FS 364 INBD OF S26R IS CORRODED. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001-A01. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED INTERCOSTAL IAW SRM 51-42-20-001-001-A01, 51-42-21-001-001-A01, AND APPLIED A023 FINISH AND CIC IAW SRM 51-25-00-001-001-A01 AND 51-21-16-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 364) · airframe 10,637 hrs · 6,991 cycles
INTERCOSTAL FWD OF FS 364 INBD S26R IS CORRODED. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED INTERCOSTAL FWD OF FS 364 S26R IAW SRM 51-42-06-0001-001-A01, 51-42-20-001-001-A01 AND 51-42-21-001-001-A01 AND APPLIED A023 FINISH AND CIC IAW 1-25-00-001-001-A01 AND 51-21-16-001-001-A01.AND DWG SH670-32050.
Part: FRAME — CORRODED (BS 319) · airframe 10,637 hrs · 6,991 cycles
FRAME BS 319 CORRODED AT THE BOTTOM. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS .050 IAW SRM 53-21-06-001-002-A01.
Part: FRAME — CORRODED (BS 349) · airframe 10,637 hrs · 6,991 cycles
FRAME BS 349 IS CORRODED AT THE BOTTOM. REPAIRED IAW SRM 51-21-06-001-001-A01.
Part: POST — CORRODED (COCKPIT DOOR) · airframe 10,637 hrs · 6,991 cycles
COCKPIT ENTRY LT DOOR POST CORRODED AT WL 72.50 AT LBL 9. REMOVED CORROSION IAW SRM 51-42-13-001-001 & 51-21-06-001-001 ORIGINAL MAT THICKNESS .032", IAW SRM 53-11-10-003-A01. COMPLIED WITH REO 690-53-11-485.
Part: FRAME — CORRODED (BS 310) · airframe 10,637 hrs · 6,991 cycles
FRAME BS 310 IS CORRODED AT THE BOTTOM. REMOVED CORROSION BS 310 BETWEEN STR 25-26R IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EO CL600-2024-53-I00181.
Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 10,637 hrs · 6,991 cycles
RT CABIN FLOOR SUPPORT AT WL 72.50 CORRODED AT FS 280.00. REPAIRED IAW RM 53-21-43-101-001-A01 AND REO 670-53-21-139.
Part: FRAME — CORRODED (BS 280) · airframe 10,637 hrs · 6,991 cycles
AT THE BOTTOM OF FRAME BS 280 THE RING BELOW THE FRAME IS CORRODED. REMOVED CORROSION FROM FS 280 BUTTSTRAP STR 26L-26R IAW SRM 51-21-06-001-001. ORIG MAT .080 IAW DWG SH670-35254. RECEIVED AND COMPLIED WITH EO IAW NDTM PT-1, 51-20-006-250-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,637 hrs · 6,991 cycles
COCKPIT FLOOR PANEL 221ALF AFT FLOORBEAM ANGLE CORRODED AT FS 280.60. REMOVED FLOORBEAM ANGLE AT BS 280.60 IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE COCKPIT FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.
Part: LIGHT — DAMAGED (CABIN) · airframe 10,637 hrs · 6,991 cycles
EMERGENCY LIGHT DAMAGED. R & R DAMAGED LIGHT IAW AMM 33-51-01-400-801.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,637 hrs · 6,991 cycles
LT 280 FLOORBEAM CORRODED AT LBL 9. R & R FS 280 LT SIDE FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND 51-41-13-001-001 DWG CC670-34094.
Part: POST — CORRODED (COCKPIT DOOR) · airframe 10,637 hrs · 6,991 cycles
COCKPIT ENTRY RT DOOR POST CORRODED AT WL 72.50 AT RBL9. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-001-A01, 51-42-06-001-001-, 51-42-13-001-001. RECEIVED AND COMPLIED WITH REO 690-53-11-487 REPAIR STEPS 1 & 2 & 3 REO 690-53-11-487.
Part: SHEAR TIE — CORRODED (BS 295) · airframe 10,637 hrs · 6,991 cycles
FRAME BS 295 BOTTOM CORRODED. REMOVED CORROSION FROM SKIN ATTACH FLANGE AT FRAME 295 IAW SRM 51-21-06-001-001-A01 & CHECK LIMITS IAW SRM 53-21-06-101-002-A02. REMOVED CORROSION AT FRAME 295 BETWEEN S26R & 26L IAW SRM 51-21-06-001-001-A01 ORIGINAL THICKNESS .050 IAW SRM 53-21-06-001-002-A01. RECEIVED AND COMPLIED WITH EO CL600-2D24-53-I00182.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,637 hrs · 6,991 cycles
RT 280 FLOORBEAM CORRODED AT RBL 9. R & R RT SIDE BS 280 FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001 DWG CC670-34094.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 10,637 hrs · 6,991 cycles
SERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED IAW SRM 51-42-06-001-001-0A1 AND 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 10,637 hrs · 6,991 cycles
RT FLOOR SUPPORT WL 72.50 CORRODED AT FS 349. REPAIRED IAW RM 51-21-06-001-001-A01 AND EO CL600-2D24-53-I00184.
2012
Part: SENSOR — MALFUNCTIONED (BRAKE SYS) · airframe 9,881 hrs · 6,529 cycles
BRAKE OVERHEAT WARNING MSG ON TAKE OFF, LT INBD BRAKE INDICATING 20 ON BTMS . ENROUTE, ACFT DIVERTED, EMERGENCY DECLARED. R & R LT INBD BRAKE TEMP SENSOR IAW AMM 32-46-01. OPS TESTED GOOD IAW AMM 32-46-01-740-801,
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 8,253 hrs · 5,500 cycles
RT OVERWING EMERGENCY LIGHT OUT. R & R OVERWING EMERGENCY LIGHT IAW AMM 33-51-15.
Part: MEGAPHONE — DAMAGED (CABIN) · airframe 7,731 hrs · 5,144 cycles
FLIGHT ATTENDANT REPORTED MEGAPHONE TEST BUTTON DAMAGED. REPLACED MEGAPHONE ASSY IAW AMM 25-61-14. OP'S CHECKED GOOD.
2011
Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 7,416 hrs · 4,969 cycles
CAPTAIN`S FLASHLIGHT IS NOT IN GOOD WORKING CONDITION. R & R CAPT FLASHLIGHT IAW AMM 25-60-00. OPS CHECK GOOD.
Part: MOTOR — FAILED (SLATS) · airframe 7,041 hrs · 4,748 cycles
ON APPROACH, RECEIVED SLATS FAIL CAUTION MESSAGE, COMPLIED WITH QRH, EMERGENCY DECLARED. MDC DISPLAY SLAT PDU MOTOR 1 FAULT, R & R SLAT MOTOR PDU MOTOR 1 IAW AMM 27-81-37, OPS CHECKED IAW AMM 27-50-00.
Part: WARNING MESSAGE — ILLUMINATED (SLATS) · airframe 7,041 hrs · 4,748 cycles
SLATS FAIL CAUTION MESSAGE ON DECENT, EMERGENCY DECLARED. CLEARED INHIBITS. PERFORMED OPS CHECK IAW AMM 27-50-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
Part: BPSU — WORN (SLATS) · airframe 6,937 hrs · 4,680 cycles
L/E SLATS FAIL MSG INFLIGHT. RAN QRH CHECKLIST AND RAN FLAPS UP, NO CHANGE. LANDED WITH FLAPS AT 45 AND NO SLATS. (EMERGENCY DECLARED AS A PRECAUTION) FOUND LT SLAT BPSU BAD. R & R LT SLAT BPSU IAW AMM 27-81-03. PERFORMED MECHANICAL AND ELECTRICAL RIGGING, OPS CHECK GOOD. ACFT OK FOR SERVICE AT THIS TIME, IPC 27-81-03 ITEM NR 5 /MX NOTIFIED RM7016773. (SDR CLOSED)
Part: DOOR — BINDING (SERVICE) · airframe 5,779 hrs · 3,912 cycles
MAIN DOOR WOULD NOT OPEN FIRST FLIGHT OF THE DAY. ENTERED CABIN SERVICE DOOR AND WAS ABLE TO OPEN IT. OPS CHECK PAX DOOR FUNCTIONS IAW AMM 52-11-00. NO DEFECT NOTED. (CLOSED)
Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 5,317 hrs · 3,585 cycles
EMERGENCY LIGHT TRACK AT GALLEY 2 HAS BROKEN COVER AND AISLE LIGHT MARKER HAS DAMAGE FROM WATER. REMOVED AND REPLACED AISLE LIGHT MARKER WITH SERVICABLE PART IAW AMM 33-51-01-000-801 AND 33-51-01-400-801.